Unconventional aircraft configurations allow obtaining better aerodynamic characteristics if intrinsic shortcomings are eliminated. The possible resolution of these shortcomings is presented using an example of a developed unmanned aerial vehicle of three lifting surface configuration featuring a new type of leading-edge vortex generators. This paper describes the effect of leading-edge vortex generators installation on the foreplane and elaborates on shortcoming resolution and gained advantages in aerodynamic characteristics. Computational Fluid Dynamics simulation results of foreplane with leading-edge vortex generators are outlined.


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    Titel :

    Aerodynamic Performance Improvement of UAV by means of Leading-Edge Vortex Generators


    Beteiligte:


    Erscheinungsdatum :

    01.10.2019


    Format / Umfang :

    388195 byte



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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